국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	A Preliminary Flight Test on a Basic Performance of the Flight Research Airplane Do 228:Velocity v.s. Glide Path Angle
저자	Yoshikazu Miyazawa, Takatsugu Ono, Yasuhito Kawagoe
Keyword
URL	http://send.nal.go.jp/send/jpn/dlpdf.php3/naltm00613.pdf?id=NALTM0000613
보고서번호	NAL TM-613
발행년도	1989.9
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	A preliminary flight test was conducted of the research airplane Dornier Do228-200 that is being modified for use as an in-flight simulator by the National Aerospace Laboratory. The basic performance of the airplane was evaluated by the flight test. Glide path angles were examined with various parameters, such as velocity, altitude, and power. The flight test results were compared with those of a mathematical model based on the Dornier GmbH wind-tunnel test data. Since an onboard data acquisition system is under development and only primiti